A Strongly-coupled Non-parametric Integral Boundary Layer Method for Aerodynamic Analysis with Free Transition
Author:
Affiliation:
1. Massachusetts Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1154
Reference38 articles.
1. Viscous-inviscid analysis of transonic and low Reynolds number airfoils
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3. Correlation-Based Transition Modeling for Unstructured Parallelized Computational Fluid Dynamics Codes
4. Computational Fluid Dynamics Compatible Transition Modeling Using an Amplification Factor Transport Equation
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